System and method for producing a hardened and tempered structural member

ABSTRACT

System and methods relating to in-line heat-treating, hardening and tempering of material, such as for example, coiled steel into a roll-formed, hardened and tempered structural member having uniform or different targeted properties in selected zones of the structural member. The different targeted properties may be achieved by heating and/or cooling the material subject to certain parameters.

CLAIM TO PRIORITY

This divisional patent application claims priority to and benefit of,under 35 U.S.C. § 121, U.S. patent application Ser. No. 14/337,921,filed Jul. 22, 2014 and titled “System And Method For Producing AHardened And Tempered Structural Member”, all of which is incorporatedby reference herein.

TECHNICAL FIELD

Generally, an in-line system and method that produces a hardened andtempered structural member is taught. More specifically, an in-linesystem and related method that utilizes rapid induction heating andrapid cooling to produce a hardened and tempered structural member withsurprisingly minimal distortions. In some embodiments the in-line systemand method produces a structural member having uniform physicalproperties, and in other embodiments a structural member is producedhaving two or more physical properties present in two or more zones.

BACKGROUND

Heating and cooling of materials, such as steel, can alter theproperties of the utilized material used to form finished products suchas structural members, including frame rails for motor vehicles such asheavy trucks. Moreover, targeted heating, cooling, other processes, orthe combination thereof can alter the properties to targeted propertiesor parameters. To this end, various processes of heating and/or coolingmaterials have been developed. However, such processes as are presentlyknown yield structural members with distortions (such as bow or camber,etc.) which are expensive time-consuming to correct. Plus, known systemsto harden and or temper metal products such as structural members haveproven costly, time consuming, and/or relatively inefficient. Finally,known systems to harden and/or temper metals such as structural membersrequire multiple pieces of equipment positioned separated from oneanother on large amounts of floor space (“foot print”) in a factory,requiring physical transfer of hot metal parts from one processingstation to another. Such physical transfer of hot metal parts presentsnot only a safety issue, but also presents opportunities to introduceadditional distortions into the product.

For example, processes to date that utilize heating as well as quenchingand/or spraying with cool water of steel generally require largefurnaces or ovens for heating and large tanks for rapid cooling, such asby spraying or quenching. As mentioned, such large equipment requires alarge amount of floor space (“foot print”) or allocation ofmanufacturing space, which can be expensive as well as inefficient.Moreover, transferring of product between such large equipment isdifficult and/or labor intensive. For example, transitioning from alarge furnace/oven in one location to a large piece of cooling orquenching equipment in a second location may require transporting thetreated equipment from one area of a manufacturing floor to another area(e.g., from a heating area to a quenching area) by fork truck, cargotruck, rail, etc., or even from one manufacturing building to another.This transportation of work pieces from one piece of processingequipment to the next piece of process equipment can be expensive and/ortime consuming, leading to increased cost of production, productiontime, and/or inefficiencies that lower productivity or profit.

Thus, there is a need in the art both for producing a hardened andtempered structural member, and for overcoming issues of existingmultiple facility or large foot print systems for producing hardened andtempered structural members with minimal distortions.

SUMMARY

The present disclosure is directed towards systems and methods forin-line hardening and tempering or treatment of materials to produce astructural member, including roll forming the material prior toinduction heating and rapidly cooling the structural material to alterthe physical properties of the material in targeted ways, includingproducing two or more physical properties in two or more zones of asingle structural member.

Optionally, in some embodiments a hardened and tempered structuralmember may be produced with uniform or symmetric physical propertiesthroughout, while in other embodiments a hardened and temperedstructural member may be produced with different physical propertieswithin a single profile, with physical properties varying in varioustargeted zones of the structural member (i.e. non-uniform orasymmetric).

Generally, in one aspect, a method for producing a hardened and temperedstructural member is disclosed. A ferrous work piece is provided androll formed into a profiled work piece of selected profile. The profiledwork piece is rapidly heated a first time in an induction heating deviceto above a first temperature, thus forming a first metallurgical phasesubstantially throughout the profiled work piece. The profiled workpiece is rapidly cooled a first time at a first rapid cooling rate fromabout the first temperature to a second temperature, thereby convertingthe first metallurgical phase to a second metallurgical phasesubstantially throughout the profiled work piece, which results in ahardened work piece still having about the selected profile. Thehardened work piece is rapidly heated in a second induction heatingdevice a second time to a third temperature, which tempers the hardenedwork piece, thereby forming a hardened and tempered work piece havingthe selected profile and a desired hardness. The hardened and temperedwork piece may be rapidly cooled a second time at a second rapid coolingrate to a fourth temperature.

Optionally, the first temperature may be in the range of about 800degrees C. to about 1000 degrees C., and may be about 950 degrees C.,and the first metallurgical phase may be austenite. The secondtemperature may be in the range of about 20-200 degrees C., the secondrapid cooling may occur in about 10 seconds or less, and the secondmetallurgical phase may be martensite. The third temperature may beabout 450 degrees C. or higher. The fourth temperature may be about 150degrees C. or less. The method may be completed in less than about 10minutes. Powder coating the hardened and tempered structural member maybe added as an additional step. The hardened and tempered structuralmember may be further roll formed or calibrated to reduce distortionstherein, before or after powder coating or other steps. Each step of themethod may occur substantially continuous and in-line in a straightline. The hardened and tempered work piece may be cut-to-length, andthis cutting-to-length may optionally be continuous and in-line with theother continuous and in-line steps, if they are continuous and in-line.The hardened and tempered structural member may be a frame rail. Thework piece may be subjected to heating and/or cooling that issubstantially symmetric. If heating and/or cooling is symmetrical,hardness may be substantially uniform across zones of the work piece,and/or distortions may be less than about 1 mm/m in the hardened andtempered work piece. Distortions may be measured by an optical device,which, if included, may include a laser. If an optical measuring deviceis included, it may continuously provide measurement information to acomputer, which may determine if there is distortion above an acceptableamount. The computer may activate a calibration device resulting infurther roll forming to get any distortions to less than the acceptableamount, which may be about 1 mm/m. The work piece may be subjected toheating, cooling, and/or tempering that is asymmetric at selected zones,which may result in a work piece having selected zones of differenthardness. A first zone may include a web, and/or a second or subsequentzone may include one or more flanges.

Generally, in another aspect, a method for producing a hardened andtempered structural member is disclosed. A coiled ferrous work piece ofselected composition is provided and roll formed into a desired profile.The ferrous frame rail is rapidly heated to within the range of about850-1000 degrees C. within about 300 seconds to produce austenitesubstantially throughout the profile of the work piece. The work pieceis rapidly cooled to below about 350 degrees C. within about 10 secondsor less to convert the austenite to martensite substantially throughoutthe work piece, resulting in a hardened work piece. The hardened workpiece is rapidly heated in a second induction heating device to about450-600 degrees C. within about 40 seconds or less to temper it,resulting in a hardened and tempered work piece having a desiredhardness in the form of, for example, a frame rail for a heavy truck.The hardened and tempered work piece may be cooled to a desired cuttingtemperature. The hardened and tempered work piece (frame rail) may becut to length as desired, for example, to an exemplary length of 8.53meters (28 feet). Using the in-line process described herein, an 8.53meter (28 foot) hardened and tempered frame rail can be producedbeginning with coiled steel to completed frame rail within about lessthan 10 minutes.

Optionally, the hardened and tempered work piece may be powder coatingduring the process. The composition of the work piece may be SAE 15B27steel. The work piece may be subjected to substantially symmetricalheating and/or cooling, which may result in minimal distortionsresulting from the heating and/or cooling. The work piece may besubjected to asymmetric heating, asymmetric cooling, and/or asymmetrictempering at selected zones of the work piece, which may result in thehardened and tempered work piece having selected zones of differinghardness. A first zone may include a web, and/or a second or subsequentzone may include one or more flanges. Each step of the process may occursubstantially continuous and in-line in a straight line, although suchan arrangement is optional. Distortions may be measured by an opticalmeasuring device (e.g., a laser) and, if so, it may continuously providemeasurement information to a computer, which may determine if there isdistortion above an acceptable amount. The computer may activate acalibration device resulting in further roll forming to get anydistortions to less than the acceptable amount, which may be about 1mm/m.

Generally, in yet another aspect, a method for producing a hardened andasymmetrically tempered structural member is taught. A steel work pieceof selected composition is provided and roll formed into a profiled workpiece. The profiled work piece is rapidly heated a first time in aninduction heating device above a first temperature within about 300seconds, at which point a first metallurgical phase is producedsubstantially throughout the profiled work piece. The profiled workpiece is rapidly cooled a first time at a first cooling rate from aboutthe first temperature to a second temperature to convert the firstmetallurgical phase to a second metallurgical phase substantiallythroughout the profiled work piece, which results in a hardened workpiece having said desired profile. The hardened work piece is heatedrapidly and asymmetrically in a second induction heating device to atleast one third temperature to asymmetrically temper the hardened workpiece and produce a hardened and tempered work piece having a pluralityof temper zones, with each temper zone having a different hardness. Thehardened and tempered work piece is rapidly cooled a second time at asecond cooling rate to a fourth temperature appropriate for cutting thehardened and tempered structural member into finished length.

Optionally, a first temper zone may include a web, and/or a second orsubsequent temper zone may include one or more flanges. Each step mayoccur substantially continuous and in-line in a straight line, ifdesired. Distortions may be measured by an optical measuring device,such as a laser. If an optical measuring device is included, it maycontinuously provide measurement information to a computer, which maydetermine if there is distortion above an acceptable amount. Thecomputer may activate a calibration device resulting in further rollforming to get any distortions to less than the acceptable amount, whichmay be about 1 mm/m.

Generally, in a further aspect, a system for in-line processing ofcoiled steel into hardened and tempered frame rails having minimaldistortions is taught. The system includes a feeder station to feed thecoiled steel to the components that sequentially process the coiledsteel into a tempered frame rail. These components include, insequential order, a first roll forming station, a first rapid heatinginduction heating apparatus, a first rapid cooling apparatus, a secondrapid heating induction heating apparatus, and a second rapid coolingstation. The first roll forming station forms the coiled steel into adesired profile. The first rapid heating induction heating apparatusheats the profiled steel above its austenitizing temperature while thesteel is fed therethrough. This converts the metallurgical profile ofthe steel work piece to austenite substantially throughout. The workpiece is fed to the first rapid cooling station which converts theaustenite to martensite, and feeds the martensitic work piece to thesecond rapid heating induction heating apparatus, which tempers the workpiece. The work piece is tempered into a hardened and tempered workpiece with a desired hardness. The hardened and tempered work piece isfed to the second rapid cooling station where it is rapidly cooled tominimize distortions therein.

Optionally, the work piece may be subjected to substantially symmetricheating at the first rapid heating induction heating apparatus and/orsymmetric cooling at the first rapid cooling apparatus. If such heatingand/or cooling is symmetric, the desired hardness achieved in thehardened and tempered work piece may be substantially uniform across aplurality of zones of the work piece, and/or distortions in the hardenedand tempered work piece may be less than about 1 mm/m. The feeder, rollforming station, both heating apparatus, and both cooling apparatus maybe substantially continuous and in-line in a straight line. The systemmay include a second roll forming station or calibration mill wheredistortions may be measured by an optical device (e.g., a laser). If anoptical measuring device is included, it may continuously providemeasurement information to a computer, and that computer may determineif there is distortion above an acceptable amount. If distortion abovethe acceptable amount is measured and/or determined to exist, acalibration device may be activated. The calibration station may includeroll formers, which may be activated by the calibration device ifunacceptably high distortions are measured and/or determined to exist,and the roll formers may reduce distortions in the work piece to lessthan the acceptable amount, which may be about 1 mm/m. The system mayinclude a cutting station wherein the hardened and tempered work piecemay be cut to a desired length.

This Summary is provided to introduce a selection of concepts in asimplified form that are further described below in the DetailedDescription. This Summary is not intended to identify key features oressential features of the claimed subject matter, nor is it intended tobe used to limit the scope of the claimed subject matter. A moreextensive presentation of features, details, utilities, and advantagesof any present embodiment is provided in the following writtendescription of various embodiments, illustrated in the accompanyingdrawings, and defined in the appended claims.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a perspective schematic view of embodiments of equipment and aprocess for in-line tempering and hardening of an exemplary work piece;

FIG. 2 is a flow chart of an exemplary in-line manufacturing process fora structural member including a tempering process;

FIG. 3A is a front view of an exemplary embodiment of a continuous workpiece of material;

FIG. 3B is a front view of an exemplary embodiment of the continuouswork piece of FIG. 3A having an intermediate process profile;

FIG. 3C is a front view of an exemplary embodiment of the continuouswork piece of material of FIG. 3B in the desired form of a structuralmember having a finished process profile;

FIG. 4 and FIG. 4A are, respectively, top and cross section (along line4A-4A) views of an embodiment of an arrangement of an exemplaryinduction heating coil acting upon the work piece during the in-lineprocess for producing a structural member;

FIG. 5 and FIG. 5A are, respectively, top and cross section (along line5A-5A) views of an alternative arrangement of an exemplary inductionheating coil acting upon the work piece during the in-line process forproducing a structural member;

FIG. 6 and FIG. 6A are, respectively, top and cross section (along line6A-6A) views of yet another arrangement of exemplary induction heatingcoils acting upon the work piece during the in-line process forproducing a structural member;

FIGS. 6B and 6C are end views of yet other arrangements of exemplaryinduction heating coils acting upon zones of the work piece;

FIG. 7A is a side of an exemplary embodiment of an induction heatingdevice and cooling/quenching nozzle acting on the continuous work piece,with the nozzle disposed to deliver its cooling spray at an angle awayfrom the induction heating device;

FIG. 7B is a front view of an exemplary embodiment of a continuous workpiece being symmetrically cooled by a plurality of spray jets acting onthe surface of the continuous work piece;

FIG. 8 is a perspective view of an exemplary embodiment of a piece ofmaterial now in the form of a structural member having the finishedprocess profile of FIG. 3C and a uniform hardness profile;

FIG. 9 is a perspective view of an exemplary embodiment of a piece ofmaterial formed into a structural member having the finished processprofile of FIG. 3C and a plurality of zones of physical properties ofthe structural member;

FIG. 10 is a front view of an embodiment of a finished work piece havingphysical properties that may vary across exemplary zones; and

FIG. 10A is a line graph showing exemplary physical properties of theexemplary zones of FIG. 10.

DETAILED DESCRIPTION

It is to be understood that the embodiments are not limited in theirapplication to the details of construction and the arrangement ofcomponents set forth in the following description or illustrated in thedrawings. Other embodiments are possible and may be practiced or carriedout in various ways. Also, it is to be understood that the phraseologyand terminology used herein is for the purpose of description and shouldnot be regarded as limiting. The use of “including,” “comprising,” or“having” and variations thereof herein is meant to encompass the itemslisted thereafter and equivalents thereof as well as additional items.Unless limited otherwise, the terms “connected” and “coupled” andvariations thereof herein are used broadly and encompass direct andindirect connections and couplings. In addition, the terms “connected”and “coupled” and variations thereof are not restricted to physical ormechanical connections or couplings.

Referring initially to all figures, embodiments of a system 10 andprocess for forming a continuous work piece 100 into a finishedstructural member 200 are depicted. Some exemplary structural members200 may be any of a variety of frame rails, such as the type commonlyused in motor vehicles or the like. The system and/or process is in-linethroughout, so that continuous work piece 100 may be linearly advancedwithout any substantial interruptions due to a substantial absence ofseparations between portions of the process or steps of the process.This continuity of process shortens process times and decreases theamount of time between processes or stages of the system. Significantamount of time between or after certain stages or process steps can leadto unwanted variability in the properties of continuous work piece 100and/or finished frame rail or structural member 200. For example, in anon-continuous process, after heating a work piece may be transferred toa rapid cooling station or process step, which presents a safety hazard.Also, during this transfer the work piece may cool in an uncontrolledand/or undesirable manner. Such uncontrolled or undesirable cooling mayresult in undesirable metallurgic or physical properties and/orgeometric distortions being present in the work piece.

Moreover, such discontinuity and/or excessive transfer or transportationprocess steps will likely result in an inefficient process, takinglonger than necessary. Furthermore, a process or system that is notin-line will require more floor space and/or a larger square footage“foot print” than will an in-line process. Thus, an in-line system canresult in a safer, smaller, more efficient process that results in anoptimized product (e.g., frame rail or structural member 200) havingdesired metallurgic properties, as well as minimal distortions withoutrequiring extra forming or hammering to remove distortions. Moreover,having the in-line system 10 arranged in a substantially straight lineor orientation may further improve efficiency, further reduce the sizeof the foot print, and/or improve results (e.g., minimize distortions),at least because a straight line orientation may reduce the geometricspace required (and/or the distance required for continuous work piece100 to travel). Furthermore, by keeping continuous work piece 100continuous, the process may allow for efficient correction of continuouswork piece 100 into final shape, form, or profile, for example, by useof conventional roll forming techniques combined with opticalmeasurement (e.g., by an optical measuring device 650) and feedback(e.g., by a computer 750) to a calibration mill (e.g., calibrationstation H, discussed below), any or all of which may occur with littleor no human oversight.

Referring now to FIG. 1, a perspective view of an exemplary in-linesystem for processing frame rail or structural member 200 from a blankcontinuous work piece 100. A system 10 provides equipment for processingthe continuous work piece 100 into structural member or frame rail 200having a selected and/or desired profile (e.g., U-shaped channel,I-shaped, Z-shaped box shaped, or other structural shape or combinationof shapes, some or all of which may be commonly used as structuralmembers including but not limited to frame rails used in, for example,motor vehicles). Structural member 200 may also have varying or constantmetallurgical characteristics or physical properties. For example, thehardness and/or brittleness, yield, elongation, elasticity, tensilestrength, and/or shear strength of frame rail or structural member 200may be altered by certain processing steps imposed on continuous workpiece 100. Continuing this example, continuous work piece 100 may bemade hard and/or brittle during a first heating and cooling cycle inwhich austenite/martensite is formed within or throughout continuouswork piece 100, and then continuous work piece 100 may be subjected to atempering process in which the hardness and/or brittleness is reduced(although in some embodiments the work piece 100 may still be harderthan before the first heating and cooling cycle and/or before martensiteis formed).

Continuous work piece 100 may be provided in any of a variety of formsor having any of a variety of compositions, including, but not limitedto, as a roll or coil of SAE 15B27 steel at a supply station A.Continuous work piece 100 may be ferrous, including iron, and/or mayinclude carbon and/or other metals or elements therewith. As usedherein, the reference character “A” may be used to denote supply stationA or the supplying step A of providing continuous work piece 100 (thesame applies for stations or steps B-I, described below). A variety ofcompositions may be used for continuous work piece 100. For example,boron-manganese steels having compositions with at least one of thealloy elements within the following approximate mass percentage ranges:

Carbon (C) 0.08-0.6,  preferably, 0.08-0.30 Manganese (Mn) 0.8-3.0,preferably, 1.00-3.00 Aluminum (Al) 0.01-0.07, preferably, 0.03-0.06Silicon (Si) 0.01-0.5,  preferably, 0.01-0.20 Chromium (Cr) 0.02-0.6, preferably, 0.02-0.30 Titanium (Ti) 0.01-0.08, preferably, 0.03-0.04Nitrogen (N) <0.02, preferably, <0.007 Boron (B) 0.002-0.02, preferably, 0.002-0.006 Phosphorus (P) <0.01, preferably, <0.01Sulfur(S) <0.01, preferably, <0.01 Molybdenum (Mo) <1,   preferably,<1.00 iron and/or impurities residual.

For example, steels including the following alloy composition have beenfound suitable for use with embodiments of system 10:

C [%] Si [%] Mn [%] P [%] S [%] Al [%] Cr [%] Ti [%] B [%] N [%] 0.220.19 1.22 0.0066 0.001 0.053 0.26 0.031 0.0025 0.0042the rest being made up of iron and inevitable smelting-relatedimpurities.

For another example, a selected form coil composition may be SAE 15B27having about 0.25-0.30% carbon, about 0.15-0.30% silicon, about1.35-1.65% manganese, about less than 0.04% phosphorus, and about lessthan 0.04% sulfur. It is understood that SAE 15B27 is merely anexemplary type or composition of steel material that may be used, andthat any of a variety of other steels may be used (e.g., the carbonand/or manganese content may vary+/−50% from the content of SAE 15B27,and/or compositions in the range of about 20 MnB5 through 30 MnB5 may beused, although these are just additional exemplary compositions), any ofa variety of other non-steel or non-metal materials may be used, or anycombination thereof. For example, aluminum and/or aluminum alloys may beused, and/or any of a variety of other metals or non-metals instead ofor in addition to aluminum or aluminum alloys may be used. It isunderstood that, although steel is discussed in detail herein, includingthe formation of austenite and martensite, such description does notlimit the materials that may be used to steel or to materials in whichaustenite or martensite may be formed. Exemplary embodiments comprisingrolled sheet steel may have a thickness in the range of about 0.5 mm to13 mm, and in some embodiments rolled sheet steel having a thickness inthe range of about 6 mm-9 mm may be used. The coil profile or shapedefines the starting profile of continuous work piece 100, which isunrolled and fed to a subsequent feeder station B using equipment wellknown in the art.

Feeder station B may be provided to supply continuous work piece 100from supply station A to subsequent steps of the process or methodand/or to subsequent portions of the system for producing structuralmember 200. In one embodiment, the feeding of continuous work piece 100through the stages of the in-line system 10 is accomplished by astandard roll-forming line as will be understood in the art. Any of avariety of feed rates may be used, without limitation, although in someembodiments feed rates in the range of about 2.5-9 meters/minute may beused. It is understood that the feed rate may be based on thelimitations of other equipment, stations, or steps in the process, suchas, for example, the power available to the first rapid heating stationD and/or the second rapid heating station F, and/or the spray rates orflow rates at first rapid cooling station E and/or the second rapidcooling station G. The feeding accomplished by roll former acting asfeeder station B may be augmented by a calibration mill H at the end ofthe process. Further, the feeding may also be assisted by driven rollsat various stages along the process flow, such driven rolls operating ina manner understood by those skilled in the art. In some embodiments,continuous work piece 100, en route to becoming structural member 200(for example along processing direction P), may be formed at rollforming step C, heated at induction heating step D, rapidly cooledand/or quenched at cooling step E, rapidly heated at tempering step F,rapidly cooled and/or quenched at cooling step G, cut and/or otherwiseprocessed in any of a variety of ways to, for example, be infused withdesired or target properties and/or to be shaped or formed as desired.Optionally, regarding the cooling step G, the work piece may be simplyallowed to cool ambiently before being calibrated at station H and thencut to length at station I.

Optionally, feeder station B may include any or all of an uncoiler (notshown), a peeler (not shown), and a flattener (not shown) to, forexample, facilitate feeding continuous work piece 100 to and/or throughsystem 10. For example, an uncoiler, if included, may process a coiledor spooled roll of material through a straight or in-line orientation. Apeeler and/or a flattener may further process continuous work piece 100into a shape or form (e.g., straightened, flattened, cleaned, and/orcleared of debris). Optionally, a cut-off device (not shown) may beincluded, for example, so that continuous work piece 100 may be cutbetween feeder station B and roll former C or subsequent station orstep, which may facilitate a safer operation and/or to prevent wasteshould there be a problem with a production run. It is understood thatany or all of an uncoiler, a peeler, a flattener, and a cut-off devicemay be separate units instead of or in addition to being included as apart of feeder station B or any other station of system 10.

The system 10 and/or process may involve or include in-line processing,which may mean that the components of the system are arrangedcontiguously in a straight line and are connected to each other allowingfor the work piece to be processed continuously from the beginningcontinuous work piece 100 (e.g., strip steel) stage to the final orstructure member 200 (e.g., a hardened and tempered frame rail) stage,without the need for collateral transfer of the work piece from oneprocessing component to the next. Use of an in-line system or processmay allow for, among other things, a smaller foot print and/or mayrequire less area for setting up or operating the system or process, amore efficient process, and/or a finished product (e.g., structuralmember 200) having minimal distortions without the need for extraforming or straightening steps.

An unexpected benefit of the in-line process of FIG. 1 is thatdistortions are minimized to a surprising degree without employing somemeans of restraint quenching as required in the prior art.

Distortion may be used to denote cross-sectional changes in continuouswork piece 100 and/or frame rail or structural member 200. For example,deviations in shape or profile of continuous work piece 100 and/orstructural member 200 (e.g., changes in angle of side flanges, ifflanges are included, or changes in thickness over the width) may bedistortions. It has been found that, with some materials and/or targetdesigns of structural member 200, less than 1 mm/m (e.g., about lessthan 0.75 mm/m) may be desirable. Distortion may be measured in any of avariety of ways, including, but not limited to, by visual inspectionand/or by tools (e.g., calipers, optical measuring systems, and/oroptical measuring device 650). In some embodiments, feedback frommeasuring may be supplied to system 10 (e.g., to a calibration mill orstraightening equipment, as is understood in the art) to make necessaryor desired adjustments to continuous work piece 100 and/or structuralmember or prior to cut off into final frame rail 200.

Optical measuring device 650 (shown schematically in FIG. 1) may includeany of a variety of optical measuring components, such as, for example,a camera, a magnifying lens, a laser, a sensor (e.g., an analog ordigital sensor), a communication device (e.g., a transceiver, a radio, acomputer, etc.), other components, or any combination thereof, includinga plurality of one or more components. Optical measuring device 650 maybe used either alone or in conjunction with other components to, amongother things, measure distortion in continuous work piece 100. Computer750 (also shown schematically in FIG. 1) may be included and/or may bein communication with optical measuring device 650, and/or may be incommunication with system 10 or any component thereof to, for example,control the feed rate of continuous work piece 100. Thus, for example,optical measuring device 650 may measure distortion(s) in continuouswork piece 100 and/or computer 750 may receive such measurementinformation and use it to determine if distortions exist that are abovean acceptable level (e.g., more than about 1 mm/m).

Computer 750 may then communicate with system 10 or components thereofto, for example, reverse or slow continuous work piece 100 for furtherprocessing and/or communicate to calibration station H to cause furtherroll forming, straightening, and/or reduction of distortion(s) untilbelow an acceptable distortion level (e.g., equal to or less than about1 mm/m). It is understood that further roll forming, straightening,and/or reduction of distortion(s) in continuous work piece 100 may berepeated as necessary, for example, by use of a feedback loop includingoptical measuring device 650, computer 750, calibration station H,and/or other components of system 10 or any combination thereof. It isfurther understood that computer 750 may be in communication with any orall stations of system 10 and/or may be used to control functionsthereof. For example, computer 750 may be in communication with feederstation B to control the feed rate of continuous work piece 100. Foranother example, computer 750 may be in communication with any of theheating stations (e.g., D and/or F) and/or in communication with any ofthe cooling stations (e.g., E and/or G) to receive temperature feedbackto adjust heating or cooling rates (e.g., as described above) and/or toadjust the feed rate of continuous work piece 100 as desired. It isunderstood that any or all communication between optical measuringdevice 650, computer 750, and/or any component of system 10 or anycombination thereof may be substantially wireless or wired, or anycombination thereof.

Fine tuning or precise control of any or process steps may minimize oreliminate unwanted distortions, for example, by fine tuning the heating,cooling, and/or tempering processes. For example, any or all of heating,cooling, and tempering steps or processes may be substantiallysymmetrical, or subjecting substantially all of a lengthwise section ofcontinuous work piece 100 to substantially the same heating or coolingrates, which may reduce thermal gradients and/or stresses, and therebyreduce distortions that may arise from uneven heating or cooling.However, it is understood that asymmetric heating, cooling, and/ortempering may be desired, in some embodiments, to give continuous workpiece 100 and/or structural member 200 variable properties, as discussedin more detail below. Moreover, distortion may be reduced or eliminatedby, for example, reducing or eliminating restraints or physical touchingof continuous work piece 100 during any or all processing steps. Furtherstill, guides, such as guide rolls or guide rails, for example, may beincluded, for example, between process steps or stations. For example,radiant cooling of continuous work piece may occur upon exit of firstrapid heating station D and/or second rapid heating station F, and thisradiant cooling may cause or increase distortions. Thus, guides may beused at these locations (or at any other location) to urge continuouswork piece to maintain its desired profile and minimize distortions.

Referring still to FIG. 1, roll forming step C is accomplished followingfeeder station B. Feeder station B, if included, may provide continuouswork piece 100 to a forming station C. Forming station C may shape orform continuous work piece 100 into a certain, predetermined, and/ordesired shape or profile (e.g., the substantially U-shaped channel shownin FIG. 1, or other shape if desired). Other shapes that profiled workpiece 150 may take include, but are not limited to, I-shape, Z-shape,box shape, or any other shape or any combination thereof. It isunderstood that continuous work piece 100 and/or structural member 200may have, without limitation, any form or shape, whether having an openshape (i.e. an open perimeter) or a closed shape (i.e. a closedperimeter, such as may be achieved by welding the perimeter shut, forexample, or by supplying a continuous work piece 100 having a closedshape or form prior to processing by system 10).

Forming station C may include any of a variety of forming methods, suchas roll forming. Roll forming may facilitate and/or efficiently shape orform continuous work piece 100 into or toward the finished profile orshape desired. For example, roll forming at forming station C mayfacilitate forming and/or efficiently form continuous work piece 100 ifcontinuous work piece 100 is steel such as SAE 15B27. If roll forming isemployed at forming station C, it may shape or form continuous workpiece 100 in a single step or in a plurality of steps in a mannerunderstood in the art. For example, a first or intermediary roll formingstep at a first pair of rollers may be followed by a final or finishingstep at a second pair of rollers. As mentioned above, exemplaryembodiments comprising rolled sheet steel may have a thickness in therange of about 0.5 mm to 13 mm, and in some embodiments rolled sheetsteel having a thickness in the range of about 6 mm-9 mm may be used.

It is understood that any number of rolling steps or pairs may beincluded, and the rollers are not limited to being in pairs. The numberof rollers and/or the orientation of rollers may be adapted as necessaryto, for example, form a finished shape or profile from a certain orpredetermined blank or beginning profile. According to present exemplaryembodiments, the continuous work piece 100 is formed by creating sideflanges in two or more steps to create the exemplary U-shaped channel.As shown in the exemplary embodiments, the flanges are turned downwardto preclude pooling of water between the web and flanges of the shapedwork piece 150 which may affect cooling and/or subsequent heating stepafter a first cooling. Once formed, continuous work piece 100 takes theform of exemplary profiled work piece 150 (for non-limiting example,channel-shaped). It is understood that profiled work piece 150 is usedto indicate a state of continuous work piece 100, and is not a separatepiece, as continuous work piece 100 is continuous throughout the in-lineprocess(es) described herein.

After being shaped or formed at forming station C the profiled workpiece 150 may be rapidly heated at exemplary first heating station D.Any of a variety of heating methods, systems, and/or apparatus may beused at first heating station D, including, but not limited to inductionheating, heating in a gas or electric oven, and/or infrared heating. Insome embodiments, induction heating may be a quick, efficient, and/orcompact heating option. One induction heating device that has proven tobe useful in this in-line process is an AJAX TOCCO Magnathermicinduction heating device, although it is understood other makes and/ormodels may be employed. Coil design and flux field are considerationsthat may be taken into account when selecting a type, make, and/or modelof heating device. The coils of the induction heating device may bemanipulated and/or formed to adapt or conform to the profile or shape ofprofiled work piece 150 that is being processed into structural member200 (see, e.g., FIGS. 4-6A, discussed below). The properties and/ormetallurgy of continuous work piece 100 may be altered, varied, and/orcontrolled by altering, varying, and/or controlling, for example, thepower to any or all coils or the spacing of the coils relative to theprofiled work piece 150. If more than one coil is included, power toeach coil may vary, for example, to create varying metallurgy inadjacent sections of continuous work piece 100. Profiled work piece 150may enter first heating station D and exit as first heated work piece160. Again, it is understood that first heated work piece 160, as usedhere, denotes the state of continuous work piece 100 at that locationalong the continuous in-line process, not a separate piece of material.

First heated work piece 160 may have certain, predetermined, and/ortarget properties that may be achieved, for example, by heating profiledwork piece 150 to a desired temperature and/or at a desired rate. Insome embodiments (possibly depending on the type of material formingcontinuous work piece 100), induction heating may be used at firstheating station D to heat continuous work piece 100 as desired in lessthan 5 minutes (300 seconds), less than about 3-4 minutes (180-240seconds) in some embodiments, or less than about 60-90 seconds in someembodiments.

Although other types of heating may be used at first heating station D,such as gas heating (e.g., in an oven) or infrared heating, inductionheating may require less space, less time, and/or less energy, and thusinduction heating may optimize process efficiency. Induction heatingmay, for example, be used to develop heat within profiled work piece 150relatively instantaneously, instead of waiting for heat to betransferred therein by conduction or convection from heat sourcesoutside profiled work piece 150. Moreover, the depth of heating may becontrolled with an induction heating device, for example, by alteringthe frequency of the current used in the induction process (whereinlower frequencies may be used to reach greater depths and higherfrequencies may be used for lesser depths). In some embodiments heatingsteel by induction, frequencies may range from about 500 Hertz to about400 kilohertz, and about 3,000 to about 10,000 Hertz has commonly foundto be an effective frequency range. The shortened time period that maybe required for induction heating (as compared to other methods ofheating) may improve accuracy and/or control of the heating process, forexample, due to reducing the time over which accidents or errorsresulting in unwanted variation of line speed, voltage, power, or otherparameters that may affect the precision of the process may occur. Insome embodiments, pyrometers or similar devices may be used during ornear the first heating process or first heating station D to collectdata and/or provide feedback, which may be used, for example, to controland/or to ensure target properties such as certain metallurgy.

Typically, profiled work piece 150 is heated to a first temperature atwhich a first hardened metallurgical phase such as austenite is formed.As will be understood by those of ordinary skill in the art, austeniteis, generally, a solid solution of carbon in iron that is stable atrelatively high temperatures. The time and temperature required toproduce the desired first metallurgical phase is controlled by a numberof parameters, such as material chemistry (e.g., steel chemistry), feedrate, power, wattage, coil positioning, range of frequencies, and powerranges of the various coils, the mass flow rate associated with theprocess, etc., as shown, for example, in the Examples set forthhereinafter. For example, first heating station D may heat continuouswork piece 100 and/or first heated work piece 160 to a first temperatureof about 950 degrees C. (or within the range of 800 degrees C. to 1000degrees C.) to be subsequently cooled, as discussed in more detailbelow. If steel is used, sufficient heat may austenitize some or all ofthe ferrite therein, changing the crystal structure from (body centeredcubic) ferrite to (face centered cubic) austenite. Ferrite typicallyexists in steel from about room temperature (or cooler) to about 720-730degrees C., at which point the ferrite begins to change to austeniteunder equilibrium conditions. Typically, in conventional gas or electricovens, the ferrite in a medium carbon steel will completely or nearlycompletely be transformed to austenite at about 850 degrees C. However,since induction heating time is typically relatively short compared toother heating methods, it has been found that raising the temperature toachieve austenitization may facilitate and/or help ensure completeaustenitization. It has been found that raising the targetaustenitization temperature about 100 degrees C. is often sufficient(e.g., from about 850 degrees C. in other heating methods to about 950degrees C., as mentioned above, in induction heating methods). Forselected steel compositions, such as SAE 15B27, continuous work piece100 may have a tempering range from about 850 degrees C. to about 1000degrees C.

First heated work piece 160 may be rapidly cooled, sprayed, and/orquenched at exemplary first rapid cooling station E and/or may exitfirst rapid cooling station E as exemplary first rapidly cooled workpiece 170 at a second temperature. Rapid cooling of austenitized steel,for example, such as may be accomplished by symmetric spraying orquenching (see, e.g., FIG. 7B), if sufficiently rapid, will transformthe austenite to (body centered tetragonal) martensite. As will beunderstood by those of ordinary skill in the art, martensite is,generally, a relatively hard and brittle solid solution of carbon iniron. If the cooling is not sufficiently rapid, the transformation fromaustenite to martensite may be incomplete or may not occur at all,and/or the austenite may instead cool slowly back into ferrite (and thusmay have ferritic properties instead of martensitic properties, whereinmartensite, for example, is generally significantly harder thanferrite). Any of a variety of cooling and/or quenching methods, systems,and/or apparatus may be used at first rapid cooling station E,including, but not limited to spray quenching (such as by spraying waterand/or emulsion, for example, onto first heated work piece 160 torapidly cool it), dipping or submerging in a pool or bath, or anycombination thereof. In some embodiments, symmetrical spray cooling hasprovided optimal cooling rates and precision, although it is notrequired to be used at first rapid cooling station E and/or in system10. Moreover, water has been found to be an efficient and economicalquenching medium for use at first rapid cooling station E. Otherexemplary quenching media may include emulsions, polymer quenchants(e.g., polyalkylene glycol), and/or other media instead of or inaddition to water. For example, emulsions and/or polymers may be addedto the sprayed water to, for example, lower the heat extraction rate,which may help minimize distortion and/or cracking of continuous workpiece 100. It is understood that it may be desirable at times to have ahigher heat extraction rate, and thus it may be desirable to spray amedium that does not have emulsions and/or polymers added thereto. Firstrapidly cooled work piece 170 may have certain, predetermined, and/ortarget properties that may be achieved, for example, by cooling orquenching first heated work piece 160 to a desired temperature and/or ata desired rate.

First rapid cooling station E may include one or more upper nozzlesand/or one or more lower nozzles, and/or one or more quench rings havingspray nozzles or features. The nozzles may be designed, located, and/ororiented to cool first heated work piece 160 with desired or targetproperties, and/or the nozzles may maintain distortion of first heatedwork piece 160 within acceptable ranges. Spray rates may be varied, anynumber of nozzles may be used, and the spray rate may vary from nozzleto nozzle, if more than one nozzle is used. In embodiments utilizing oneor more nozzles, location of the nozzle(s) as close the exit of firstheating station D as possible (e.g., as close to the final austenitizingcoil as possible) may be beneficial. For example, locating the nozzle(s)less than about 30 cm, or within about 15 cm in some embodiments, fromthe exit and/or final austenitizing coil of first heating station D maybe desirable for any of a variety of reasons, including, but not limitedto, improved control and/or precision of the cooling, quenching, and/ormartensite producing process(es). The spray nozzle(s) at first rapidcooling station E, if included, may have respective nozzle axes N₁-N₄,any or all of which may be oriented between 0 and 90 degrees, and/or atabout 45 degrees, away from first rapid heating station D. Orientingnozzles 500 as such may, for example, help overcome vapor pressure fromexcessively building up during the rapid cooling process in order tomaintain desired heat transfer and to optimally form martensite, and/orsuch orientation of nozzles 500 may reduce or prevent spray from gettingfirst heating station D or any component thereof (e.g., heating coil(s)or electrical components) wet. It is understood that the preciseorientation of nozzles 500 and/or any or all nozzle axes N₁-N₄ maydepend on a number of factors, including, but not limited to, locationof first rapid heating station D relative to first rapid cooling stationE, the composition and/or thermodynamic properties of continuous workpiece 100, and/or the target metallurgical profiles and/or physicalproperties of continuous work piece 100. If desired, coolant, such aswater, may be provided to first rapid cooling station E and/or nozzle(s)500 by or from by or from one or more sources (e.g., first storage tank550 and/or second storage tank 560). Storage tanks 550, 560 are merelyexemplary and provided as one example of how coolant and/or water may besupplied or provided.

Exemplary spray at first rapid cooling station E may be in the range ofabout 20-50 degrees C. If used, for example, in an eight nozzleconfiguration having the spray rate(s) described above, continuous workpiece 100 (depending on size, shape, material, etc.) may be cooled fromabout 950 degrees C. down to a second temperature (within the range ofabout 20-200 degrees C.), within about 10 seconds. For some materialcompositions of continuous work piece 100, cooling to about 150 degreesC. within about 10 seconds may be needed to create or form desiredproperties (e.g., a martensitic state) within continuous work piece 100.Cooling or quenching, for example, through the use of nozzles, may besubstantially symmetrical or substantially uniform across continuouswork piece 100 as measured in the axial direction and/or the transversedirection. Alternatively, cooling or quenching may be substantiallyasymmetrical, with different areas or zones of continuous work piece 100having varying metallurgic properties resulting from varying cooling orquenching (e.g., due to variant cooling rates, liquid types, nozzledesign or orientation, varying spray rates, or any combination thereof).It is understood that the rate of cooling and/or the end temperature forfirst rapidly cooled work piece 170 may be dependent on the heating thatoccurs at first heating station D, or may be independent of the heatingthat occurs at first heating station D. It is further understood that auniform, even, and/or steady flow (and/or use of maximized hole densityin the spray nozzle(s)) from each nozzle may help, for example, tooptimize cooling control and/or precision.

First rapidly cooled work piece 170 may enter rapid heating or temperingstation F (which in some embodiments may be a second induction heatingdevice similar to induction heating station D) and/or may exit temperingstation F as, for example, hardened and tempered work piece 180.Tempering station F may provide tempering of first rapidly cooled workpiece 170, and such tempering may include heat treating of first rapidlycooled work piece 170 (again, 170 is reference to a section or state ofcontinuous work piece 100 at a particular location along in-lineprocess, not a separate work piece) to increase the toughness ofcontinuous work piece 100 and/or final structural member 200. Hardenedand tempered work piece 180 may have certain, predetermined, and/ortarget properties that may be achieved, for example, by heating firstrapidly cooled work piece 170 to a desired temperature and/or at adesired rate to produce a tempered metallurgical profile. It isunderstood that the rate of heating and/or the end temperature forhardened and tempered heated work piece 180 may be dependent on theheating that occurs at first heating station D and/or the quenching orcooling that occurs at first rapid cooling station E, or may beindependent of any heating or cooling that previously occurs.

Any of a variety of heating methods, systems, and/or apparatus may beused at tempering station F, including, but not limited to inductionheating. Although any of a variety of types and/or combinations ofheating may be used at tempering station F, such as gas or electricheating (e.g., in an oven) or infrared heating, induction heating mayrequire less space, less time, and/or less energy, and thus inductionheating may optimize process efficiency. Moreover, the shortened timeperiod that may be required for induction heating (as compared to othermethods of heating) may improve accuracy and/or control of the heatingprocess, for example, due to reducing the time over which accidents orerrors resulting in unwanted variation of line speed, voltage, power, orother parameters that may affect the precision of the process may occur.Furthermore, since tempering may require a relatively high heating rate(i.e. a lot of heat input quickly), even a slight variation in a targetheating parameter (e.g., line speed or power) may have a significant,and possibly detrimental, impact on the tempering of continuous workpiece 100.

In some embodiments, for example, using steels of the compositionsmentioned above, the tempering step and/or tempering station F may raisethe temperature of continuous work piece 100 about 250 degrees C. (from,for example, about 150-200 degrees C. as it may leave first rapidcooling station E) to a third temperature in the range of about 450-600degrees C., within about less than a minute. In some embodiments,pyrometers (shown schematically as 250) or similar devices may be usedduring or near the tempering process or tempering station F to collectdata and/or provide feedback, which may be used, for example, to controland/or to ensure target properties such as certain metallurgy. Temperingstation F may include one or more heating elements and/or coils. Theproperties and/or metallurgy of continuous work piece 100 may bealtered, varied, and/or controlled by altering, varying, and/orcontrolling, for example, the power to any or all coils. If more thanone coil is included, power to each coil may vary, for example, tocreate varying metallurgy or temperatures in adjacent sections ofcontinuous work piece 100.

Hardened and tempered work piece 180 may be rapidly cooled and/orquenched at exemplary second rapid cooling station G and/or may exitsecond rapid cooling station G as exemplary tempered and cooled workpiece 190. Tempered and cooled work piece 190 may be used to form ahardened and tempered frame rail, such as hardened and temperedstructural member or frame rail 200. Any of a variety of cooling and/orquenching methods, systems, and/or apparatus may be used at second rapidcooling station G, including, but not limited to spray quenching such asby spraying water, for example, onto hardened and tempered work piece180 to rapidly cool it. Second rapid cooling station or step G may beincluded for any of a variety of reasons, including, but not limited to,making continuous work piece 100 safer to handle, to increase thedimensional stability of continuous work piece 100, and/or to reduce ordraw out residual thermal stress(es). If continuous work piece 100 israpidly cooled at second rapid cooling station G, then subsequentprocessing, forming, and/or shaping steps (e.g., further roll forming,straightening, calibrating, and/or cutting to length) can be performedwithout further distortion resulting from a hot continuous work piece100 cooling later in the process and/or cooling asymmetrically ornon-uniformly.

Tempered and cooled work piece 190 may have certain, predetermined,and/or target properties that may be achieved, for example, by rapidlycooling or quenching hardened and tempered work piece 180 to a desiredtemperature and/or at a desired rate to produce a substantially uniformmetallurgical profile. It is understood that the rate of cooling and/orthe end temperature for hardened and tempered and cooled work piece 190may be dependent on the heating that occurs at first heating station Dand/or at second heating station, and/or the cooling that occurs atfirst rapid cooling station E, or may be independent of any heating orcooling that previously occurs. It is understood that second rapidcooling station and/or second rapid cooling step G is optional. Forexample, ambient cooling and/or ambient air temperatures may be used tocontinuous work piece 100 after it has been tempered. However, it isunderstood that, in some embodiments, use of a rapid cooling station orprocess step after tempering may allow for use of a smaller foot printbecause less product will need to be cooled simultaneously, and/or itmay allow for a quicker or more efficient process or system 10.

Spray rates may be varied, any number of nozzles may be used, and thespray rate may vary from nozzle to nozzle, if more than one nozzle isused. The spray nozzle(s) 500 at rapid cooling station G, if included,may have respective nozzle axes N₅-N₈, any or all of which may beoriented between 0 and 90 degrees, and/or at about 45 degrees, away fromtempering station F. Orienting nozzles 500 as such may, for example, bedone in such a way to overcome vapor pressure from excessively buildingup during the rapid cooling process in order to maintain desired heattransfer, and/or such orientation of nozzles 500 may reduce or preventspray from getting second rapid heating or tempering station F or anycomponent thereof (e.g., heating coil(s) or electrical components) wet.It is understood that the precise orientation of nozzles 500 and/or anyor all nozzle axes N₅-N₈ may depend on a number of factors, including,but not limited to, location of tempering station F relative to firstrapid cooling station E, the composition and/or thermodynamic propertiesof continuous work piece 100, and/or the target physical properties ofcontinuous work piece 100. If desired, coolant, such as water, may beprovided to second rapid cooling station G and/or nozzle(s) 500 by orfrom one or more sources (e.g., first storage tank 550 and/or secondstorage tank 560). Storage tanks 550, 560 are merely exemplary andprovided as one example of how coolant and/or water may be supplied orprovided.

Moreover, in some embodiments, second rapid cooling station G may notsignificantly impact or alter the metallurgy or continuous work piece100 (e.g., changing from austenite to martensite as in some exemplaryembodiments of first heating station D and first rapid cooling stationE), and thus may allow for more variability and/or less precision. Forexample, second rapid cooling station G may cool continuous work piece100 to a temperature that is appropriate for subsequent handling ortreatment (e.g., painting, levelling, calibration, powder coating, orother treatment, or any combination thereof). Continuing this example,second rapid cooling station G may cool continuous work piece 100 to anexemplary fourth temperature of about 150 degrees C. or less, and/or toabout 40 degrees C. or less. The fourth temperature, or cuttingtemperature, may be sufficiently low to, for example, cut or allowcutting of continuous work piece 100 without adding more than nominaldistortions thereto.

The substantially continuous, in-line process described herein may allowfor a smaller foot print, taking up less manufacturing floor space, atleast due to the elimination or reduction of transportation of the workpiece from station to station (or process to process). This continuous,in-line process allows continuous work piece 100 to move directly fromone station to the next. This continuous, in-line process is also moreefficient as a result of this direct transfer, as unwanted oruncontrolled changes in temperature between stations is minimized, ifnot altogether eliminated. Moreover, the minimization or elimination ofsuch unwanted or uncontrolled temperature changes (and/or associatedproperty changes) has unexpectedly and surprisingly resulted inminimized distortions that would otherwise form in the work piece and/orthe finished product. Thus, use of this continuous, in-line process mayeliminate or minimize the need for post-process forming, hammering,and/or shaping of the work piece. Furthermore, variation of one or moresteps of the process described herein, and/or variation of parameters atone or more station A-I may allow for variation of the properties offrame rail or structural member 200. Further still, such variation mayoccur within a single continuous work piece 100 to cause variableproperties within a single continuous work piece 100 and/or a singlestructural member 100 varying the parameters at one or more station A-Ior one or more processing step (e.g., heating, cooling, tempering,and/or forming).

In some embodiments, tempered and cooled work piece 190 may betransported down the line, for example, by or through calibrationstation H to cutting station I, which may cut tempered and cooled workpiece 190 to length resulting in the exemplary frame rail or structuralmember 200 shown. Calibration station H may be included, for example, tomeasure and/or further process continuous work piece 100 before it iscut to length. Calibration station may include, for example, measuringequipment to find distortions or profile deviation in continuous workpiece 100 and/or to further roll form, straighten, and/or shapecontinuous work piece 100. It is understood that calibration station Hand cutting station I are optional and exemplary only. It is furtherunderstood that calibration station H and/or cutting station I may beincluded at virtually any stage along processing direction P instead ofor in addition to the locations shown. For example, in some embodimentslocation of cutting station I and/or calibration station H after formingstation C and/or before any heating or cooling occurs may be desirable,for example if an error occurs and the process needs to be ended and/orre-started. Calibration station H may include any of a variety ofhandling devices or processes, including, but not limited to, conveyers,rollers, belts, or any guide or transport device, or any combinationthereof. Cutting station I may include any of a variety of devices orprocesses for cutting structural member 200 to length, including, butnot limited to, blades, saws, torches (e.g., blow torches), or hydraulicor plasma cutting implements, or any combination thereof. Optionally, astation may be added or included for powder coating or otherwise coatingstructural member 200, for example frame rail or at any time during orafter process P. It is understood that any of a variety of other stepsor system components may be added or substituted.

Referring now to FIG. 2, a flowchart is depicted showing the steps of amethod carried out through use of exemplary system 10 of FIG. 1.Progressing in the process direction P shown in FIG. 1, which may bemodified as desired, the feeder step B may occur (e.g., as describedabove) to provide continuous work piece to the roll forming step Cand/or to subsequent steps. Continuous work piece 100 may be formed orshaped as desired prior to being heated, cooled, or tempered, which mayfacilitate and/or improve the efficiency of shaping or formingcontinuous work piece 100. After forming continuous work piece 100 intoa desired shape or profile, it may be heated, such as by inductionheating step D. As described above, the first or subsequent heating orinduction heating steps or stations may be designed and/or controlled toimpart to the work piece certain targeted properties, which may work inconjunction with the first or subsequent cooling or quenching step(s) togive the work piece certain, desired, and/or target properties. Forexample, if continuous work piece 100 is steel of the type SAE 15B27,heating the steel to a substantially high temperature in the firstinduction heating step may form austenite (e.g., by heating to or aboveabout 900 degrees Celsius). Continuing this example, rapidly cooling the(austenitic) steel in the first rapid cooling step E may result in theformation or production of martensite, which may be formed substantiallythroughout the material and/or result in substantially hardenedmaterial. The martensitic continuous work piece 100 may then be temperedat tempering station F to decrease the hardness, increase the toughness,and/or increase the workability of continuous work piece 100, forexample, as described above (e.g., may be targeted, symmetric,asymmetric, etc.). Optionally, a second rapid cooling, spraying, and/orquenching step G may occur at second rapid cooling station G for any ofa variety of reasons, including, but not limited to, cooling continuouswork piece 100 to a temperature conducive for handling and/or to furtheralter its material properties. For example, second rapid cooling step Gmay cool continuous work piece 100 to a temperature that is safe tohandle and that has minimal or no residual thermal stress prior toreaching a calibrating step H. Calibrating step H may, for example,include measuring, further shaping (e.g., by further roll forming and/orstraightening) to more precisely shape continuous work piece 100 (e.g.,within given tolerances) and/or to remove or minimize distortions.Cut-to-length step I may, in some embodiments, be included to cutcontinuous work piece 100 to length to form a finished product such asstructural member or frame rail 200. It is understood that other processsteps may be added, such as, for example, powder coating continuous workpiece 100 and/or frame rail 200. Powder coating, if it occurs, may occurvirtually anywhere, but in some embodiments may occur after calibratestep H (if included) and/or after cut-to-length step I (if included).

Subsequent heating and/or cooling of the material may occur for any of avariety of reasons. Continuing the above example in which martensite isformed, a second stage of heating may occur to temper the (martensitic)steel. For example, heating to about the range of 400-450 degreesCelsius may substantially temper the steel and/or make it more workableand/or give it desired properties (e.g., hardness and/or brittleness,yield, elongation, elasticity, tensile strength, and/or shear strength).It is understood that martensitic steel can be very hard or brittle, andoften may be difficult to work, shape, form, cut, etc. A second orsubsequent cooling stage may be included for any of a variety ofreasons, including, but not limited to, cooling the tempered steel toremove and/or minimize distortions therein.

Referring now to FIGS. 3A-3C, exemplary embodiments are shownillustrating an exemplary progression of shaping an exemplary continuouswork piece 100 having the profile shown in FIG. 3A, into an intermediateprofile shown in FIG. 3B (which may occur after shaping or formingbegins such as at a first pair of rollers, but before the final stage ofshaping or forming occurs if there is a second or subsequent stage ofshaping such as at a second pair of rollers). In some embodiments, someor substantially all forming or shaping that occurs during exemplaryprocess P may occur before any or all heating and/or cooling occurs. Forexample, if continuous work piece 100 is steel, it may be difficult toroll form or otherwise form the material after heating or cooling hasoccurred (e.g., it may be difficult to form first heated work piece 160,first rapidly cooled work piece 170, hardened and tempered work piece180, and/or tempered and cooled work piece 190, and thus may be easierto form or cut the work piece as continuous work piece 100, as profiledwork piece 150, and/or any other work piece state prior to substantialheating, cooling, and/or quenching). Thus, in some embodiments, framerail or structural member 200 may take its final shape, or substantiallyits final shape, as profiled work piece 150, prior to the first stage ofheating or cooling, such as occurs at first heating station D resultingin first heated work piece 160.

Referring now to FIGS. 4 and 4A, an embodiment of an exemplary inductionheating coil 410 is illustrated. FIGS. 5 and 5A show alternativeembodiments of an induction heating coil 420 that may be used instead ofor in addition to the induction heating coil 410 of FIGS. 4 and 4A. Asillustrated in FIG. 4A, coil 410 may be substantially rectangular toallow continuous work piece 100 to pass therethrough while being heatedby coil 410. It may also be appreciated that coil 410 is shaped in a waythat may allow various shapes of continuous work piece 100 to passtherethrough, such as, for example, a box shaped channel, an I-shaped orZ-shaped channel, and/or or any of a variety of other shapes or profilesof continuous work piece 100. Thus, coil 410 may be shaped to heat andallow passage of a variety of shapes of continuous work piece 100. Asillustrated in FIG. 5A, coil 420 may more closely track or resemble theshape or profile of continuous work piece 100. In doing so, coil 420 maybe located more closely to substantially all surfaces of continuous workpiece 100 and thereby heat continuous work piece 100 quickly and/or moreefficiently. However, it may be appreciated that coil 420 is shaped in away that may not easily allow heating and/or passage of various othershapes of continuous work piece 100, such as, for example, if continuouswork piece 100 is box shaped or Z-shaped. Either or both of coils 410may uniformly or symmetrically heat continuous work piece 100, forexample, by being substantially symmetrically disposed about continuouswork piece 100. Moreover, any number of coils 410, or of coils 420, orof both, may be used any virtually any combination.

FIGS. 6 and 6A-6C show embodiments of trim induction heating trim coils430, 432, 434, and 436 that may be used instead of or in addition to theinduction heating coils of FIGS. 4 and 4A or FIGS. 5 and 5A. Trimheating coils 430, 432, 434, and/or 436 may be used, for example, toprecisely heat continuous work piece 100 or zones thereof to achievedesired temperatures or properties (e.g., hardness, strength,metallurgical profile) of continuous work piece 100. Certain sections,portions, or zones of continuous work piece 100 may be targeted by trimcoils 432 and 434. For example, a first side trim coil 432 may targetone side or flange of continuous work piece 100 and/or a second sidetrim coil 434 may target another or opposite side or flange ofcontinuous work piece 100. In this way, a first zone or flange ofcontinuous work piece 100 may be heated differently and/or be formedwith a different hardness or other property than a second zone or flangeof continuous work piece 100. For example, the shapes of, positions of,distances from continuous work piece 100, powers to, and/or frequenciesof powers to, first side trim coil 432 and second side trim coil 434 maybe varied to result in different heating of respective zones ofcontinuous work piece 100. It is understood that the zones referred toherein may include joints, corners, any portion thereof, or anycombination thereof, instead of, or in addition to web zones and/orflange zones.

Any or all trim coils 430, 432, 434, and 436 may be used, for example,at second rapid heating or tempering station F. The various shapes,sizes, and locations relative to continuous work piece 100 of theinduction heating coils may be used to target areas or zones ofcontinuous work piece 100. In this way, the induction heating coils maybe used to rapidly heat and/or temper continuous work piece 100substantially symmetrically or uniformly, or alternatively, may be usedto rapidly heat and/or temper continuous work piece 100 substantiallyasymmetrically or non-uniformly. For example, coils 432 and 434 maytarget different sides of continuous work piece 100 to heat or temperdifferent areas at different rates and/or to different temperatures,which may result in lateral zones of continuous work piece 100 havingdifferent hardness, different strength, other different physicalproperties, or any combination thereof. Moreover, as described above,power may be varied to the respective heating coils to allow targetedheating rates and/or target heating temperatures. Thus, a continuouswork piece 100 may have a plurality of zones, any or all of which mayhave properties that are unique and/or different from any other zone(such as is illustrated in FIG. 9). In some embodiments, coil 410 may beused in conjunction with any or all trim coils 430, 432, 434, and/or436; coil 420 may be used in conjunction with any or all trim coils 430,432, 434, and/or 436; and/or coils 410 and 420 may be used inconjunction with trim coils 430, 432, 434, and/or 436.

Induction heating may be varied, controlled, and/or targeted by varyingthe shape of, power to, frequency of power to, any or all coils, such ascoils 410, 420, 430, 432, 434, and/or 436, such as described above. Anyor all heating coils, such as heating coils 410, 420, 430 may havevarious profile shapes (as shown in FIGS. 4A, 5A, and 6A). The design ofheating coils 410, 420, 430 may affect the heating rate and/or heatingefficiency. It has been found that the heating rate and efficiency maybe optimized and/or maximized by locating heating coils 410, 420, 430closely to continuous work piece 100. Keeping the inner diameter orperimeters of heating coils 410, 420, 430 and the outer perimeter ofcontinuous work piece 100 to a practical minimum may generally increaseor improve heating rate and/or heating efficiency. However, sinceheating coils 410, 420, 430 may be expensive, some compromise may bemade so that relatively few coils may be used to cover a relativelylarge range of sizes, shapes, and/or configurations of continuous workpiece 100. Typical clearances between continuous work piece 100 andcoils 410, 420, 430 may be in the range of about 3 mm to about 25 mm.Moreover, higher temperatures generally require less heating time andlower temperatures generally require more heating time. Thus, longercoils and/or more coils typically will provide more heating time, whichmay allow use of lower temperatures (and thus lower power requirementsper coil). Similar induction heating coils may be used in first rapidheating station D, and the aforementioned parameters and considerationsmay apply to such heating coils. Thus, heating may be targeted and/orvaried in first rapid heating station D, and the heating that occurs infirst rapid heating station D may be substantially symmetrical orasymmetrical.

Any or all trim coils 430, 432, 434, and 436 may take any of a varietyof shapes, forms and/or sizes. For example, they may be flat, and exertthe magnetic field over one surface or surfaces of continuous work piece100, and/or any or all coils may be contoured to wrap around the surfaceof continuous work piece 100. It has been found that it is not alwaysnecessary to have any trim coil surrounding or facing both inside andoutside surfaces of continuous work piece 100 as the heat may penetratethrough relatively thin depths of continuous work piece 100. It isunderstood that having any or all trim coils 430, 432, 434, or 436 (orother shape, size, or form) surround or face both inside and outsidesurfaces (or any other surfaces) of continuous work piece 100 mayfacilitate heating continuous work piece 100 quickly and/or efficiently,although it is not always required and/or for some shapes of continuouswork piece 100 may be of little or no additional benefit concerning timeor efficiency.

Various shapes or forms that may be used for any or all trim coils 430,432, 434, or 436 (or any other coil described herein or any other coilthat may be used) may include, without limitation, hairpin coils and/orpancake coils, as one of ordinary skill in the art will readilyappreciate and understand. A pancake coil may a plurality of distinctcoils (e.g., three distinct coils as illustrated in FIG. 6A), any ofwhich may be varied to produce a plurality of distinct heating ortempering zones. Any or all of the distinct pancake coils may be turnedon and off (or ramped up and down in power, frequency, etc.) atappropriate times as continuous work piece 100 passes under the coil(s),for example, to vary the properties (e.g., hardness, strength(s), etc.)along the length and/or width of continuous work piece 100. Thus, insome embodiments, making a straight, uniform part may require the sameequipment and capability as making a curved, non-uniform part.

I have also included a drawing from page 214 from the same referencebook. This shows the direction of the magnetic flux created by the“solenoid” coil and the pancake (or hairpin) coil. The selection of theshape coil, the frequency and the power of the coil, etc., all worktogether to influence the outcome of the process. There are variouscombinations of these factors which can produce quite similar results,and each combination may have their unique associated positive andnegative factors.

Referring now to FIGS. 7A and 7B, a plurality of sprays S from nozzle(s)500 may be directed toward or onto continuous work piece 100, such asfrom, for example, nozzle N₁ at a variety of spray angles θ₁, θ₂, θ₃.Continuous work piece 100 may move relative to first rapid heatingstation D and/or spray(s) S in process direction P. It is understoodthat more than one nozzle may be used instead of or in addition tonozzle N₁, but only one nozzle is shown in FIG. 7A for the purpose ofclarity and description. Nozzle N₁ may be oriented at impingement angleor spray angle θ₁, which is shown as about 45 degrees but may be between0 and 90 degrees, to, for example, prevent or inhibit spray S fromentering or damaging first rapid heating station D or second rapidheating station F. Spray angle θ₂ is shown at about 60 degrees, but maybe between 0 and 90 degrees, and spray angle θ₃ is shown at about 30degrees, but may be between 0 and 90 degrees. In some embodiments,sprays S may substantially surround and/or come into contact withcontinuous work piece 100 substantially uniformly at points or areasaround continuous work piece 100. Such uniformity of sprays S, and/oruniformity of spray rates and cooling media of sprays S, may facilitatesubstantially symmetrical cooling of continuous work piece 100, whichmay help minimize or prevent distortions, for example, due to gradientcooling rates and/or differing thermal stresses or if the spray nozzles500 are not all equidistant from the surface(s) of continuous work piece100. It is understood however, that sprays S may be varied to, forexample, achieve asymmetrical cooling as discussed above.

Referring now to FIGS. 8 and 9, structural member 200 may have alengthwise or axial dimension L and/or a crosswise or transversedimension T. In some embodiments, structural member may havesubstantially uniform properties (e.g., from uniform heating, cooling,and/or tempering) in axial dimension A and/or in transverse dimension T.In alternative embodiments, targeted heating and/or cooling may providestructural member 200 with various properties in the axial dimension Land/or in the transverse dimension T. For example, exemplary Zone 1,Zone 2, and/or Zone 3 may have varying metallurgical profiles,thermodynamic properties, and/or physical properties such as hardness orstrength. Thus, for example, if first rapid heating D, first rapidcooling E, and/or second rapid cooling G are substantially symmetrical,and second rapid heating or tempering F is asymmetrical (e.g., asdiscussed above and/or asymmetrical by varying power to heating coils ortargeting sides or areas of continuous work piece 100), then Zones 1-3may represent various temper zones, wherein the properties of continuouswork piece 100 and/or frame rail or structural member 200 aresubstantially varied by asymmetrical tempering at second rapid heatingstation F. It is understood that second rapid heating F may besubstantially symmetrical instead, and/or that first rapid heating D,first rapid cooling E, and/or second rapid cooling G may besubstantially asymmetrical. Asymmetric tempering resulting in varyingtemper zones in merely one example of how the properties of continuouswork piece 100 and/or structural member 200 may be varied between zones.

It is understood that, although FIG. 9 shows three zones, wherein Zone 1is the web (or a portion thereof) of continuous work piece 100, andZones 2 and 3 are respective flanges (or portions thereof) of continuouswork piece, three zones is merely an exemplary number of zones that maybe included, and one or more zones may be included instead of or inaddition to exemplary Zones 1-3. For example, temper zones and/or zonesof specified properties (whether symmetric or asymmetric) may be locatedat or near joints and/or corners where web and flange(s) meet (ifcontinuous work piece 100 includes web and flange(s)). For anotherexample, any of Zones 1-3 (or any other zone) may be further dividedinto more zones, such as, for example, is illustrated in FIG. 11. TheZones 1-3 of FIG. 9 are merely exemplary and provided for illustrativepurposes.

In some embodiments, Zone 1 may represent a central portion or web ofcontinuous work piece 100, and/or Zones 1 and 2 may represent oppositesides or flanges of continuous work piece 100. As discussed in moredetail below, the properties of continuous work piece 100 may vary fromzone to zone, or may be substantially uniform from zone to zone. Forexample, Zone 1 may be harder than Zones 2 and 3, which may be ofsimilar hardness, resulting in the “hard web” design illustrated in FIG.11. For another example, Zone 1 may be less hard than Zones 2 and 3,which may be of similar hardness, resulting in the “soft web” designillustrated in FIG. 11. For yet another example, Zones 1-3 may be ofsimilar hardness resulting in the “uniform” design illustrated in FIG.11. It is understood that other examples are possible, and that theseexamples are provided merely for the purpose of illustration. It isfurther understood that, in some embodiments, continuous work piece 100and/or structural member 200 may be formed such that Zones 1 and 2 areof dissimilar or non-uniform hardness.

It is understood that, any point prior to being formed into structuralmember 200 and/or cut such as at exemplary cutting station I, thematerial may have sufficient length in the axial dimension A to besimultaneously located in one or more stations. For example, asubstantially solid piece of material may simultaneously be in allstations prior to or including cutting station I (wherever it may belocated), such as, for example, being in each of supply station A,feeder station B, forming station C, first heating station D, firstrapid cooling station E, second heating station F, second rapid coolingstation G, calibration station H, and/or cutting station I. Thus, it ispossible that a single piece of material may simultaneously be in morethan one processing station and/or subject to more than one processingstep, although it is not required to be. Instead, it is also possiblethat a given piece of material is in only one processing station and/orsubject to only one processing step, if so desired.

With reference now to FIGS. 10 and 10A, an exemplary embodiment ofstructural member 200 is depicted having a plurality of lateral ortransverse zones Z₁-Z₇, with the Brinell hardness variable across thezones for various exemplary materials depicted by the different lines inthe chart of FIG. 10A. It is understood that structural member 200 mayhave seven zones as depicted in FIGS. 10 and 10A, may have less thanseven zones (e.g., as depicted in FIG. 9), or may have more than sevenzones. Seven zones Z₁-Z₇ are merely exemplary and provided forillustration. The differing hardness between transverse zones Z₁-Z₇ may,for example, be desired for a certain frame rail or structural member200, which may be designed for a certain use within, for example, amotor vehicle. The differing hardness between transverse zones Z₁-Z₇may, for example, be caused by targeted heating in rapid heating ortempering station F to achieve differing physical properties between thezones Z₁-Z₇ (which properties may also be varied longitudinally asdiscussed above and shown in FIG. 9, but not shown in FIGS. 10 and 11).

Examples of structural members 200, for example frame rails, havingvarious properties resulting from system 10 and/or the process describedabove are described below:

Example 1

A continuous work piece was austenitized using a single induction coilthat closely tracked the profile of the work piece (see, e.g., FIG. 5A)at 78% power of a 25 Khz 150 KW power source. The work piece was heatedin the first rapid heating station to a temperature of about 950 degreesC. The work piece was travelling at 0.73 meters/minute, and quenchedwithin about 5-10 seconds to below 100 C to create a full martensiticmicrostructure. The work piece was then tempered with the same typeinduction coil operating at 21.25% power, achieving about 510 degrees C.and travelling at 0.73 meters/minute. The work piece was then ambientair cooled over a 2 hour period. The resulting hardness of the materialwas a Brinell Hv3000 kg of 348. The resulting work piece had a tensilestrength (T) of 146.51 MPa.

Example 2

In a second example, a work piece was austenitized and tempered usingthe same process as in Example 1, except that instead of being aircooled after tempering, it was rapidly water-cooled to below 30 degreesC. The resulting hardness of the material was a Brinell Hv3000 kg of369. The resulting work piece had a tensile strength (T) of 146.51 MPa.

Example 3

In a third example, a work piece was austenitized as in Examples 1 and2, but tempered using a single induction coil having an oval shape (see,e.g., FIG. 4A) at 14% power of a 1 Khz, 250 KW induction power supply.The work piece tempering temperature was about 537 degrees C. Theresulting work piece hardness was Brinell 302 near the center (see,e.g., zone Z₄ of FIG. 10), and Brinell 287 at the flange (see, e.g.,zone Z₂ of FIG. 10). The resulting work piece had a tensile strength (T)of 96.53 MPa.

Example 4

In a fourth example, a work piece was austenitized as in the aboveexamples, but tempered using a 35 KW line induction coil having an ovalshape (see, e.g., FIG. 4A) at 12.8% power. The resulting temperingtemperature was 582 degrees C. The resulting work piece hardness wasBrinell 286 near the center (see, e.g., zone Z₄ of FIG. 10), and Brinell302 at the flange (see, e.g., zone Z₂ of FIG. 10). The resulting workpiece had a tensile strength (T) of 88.25 MPa.

Examples 3 and 4 illustrate the result of using a single coil toasymmetrically heat the work piece resulting in a zone(s) ofintentionally reduced hardness.

It is understood that the above examples are provided only for thepurpose of illustrating exemplary outcomes of the process, system, andapparatus described above, and these examples in no way limit the scopeor breadth of the claims or the description contained herein.

While several embodiments have been described and illustrated herein,those of ordinary skill in the art will readily envision a variety ofother means and/or structures for performing the function and/orobtaining the results and/or one or more of the advantages describedherein, and each of such variations and/or modifications is deemed to bewithin the scope of the embodiments described herein. More generally,those skilled in the art will readily appreciate that all parameters,dimensions, materials, and configurations described herein are meant tobe exemplary and that the actual parameters, dimensions, materials,and/or configurations will depend upon the specific application orapplications for which the teachings is/are used. Those skilled in theart will recognize, or be able to ascertain using no more than routineexperimentation, many equivalents to the specific embodiments describedherein. It is, therefore, to be understood that the foregoingembodiments are presented by way of example only and that, within thescope of the appended claims and equivalents thereto, embodiments may bepracticed otherwise than as specifically described and claimed.Embodiments of the present disclosure are directed to each individualfeature, system, article, material, kit, and/or method described herein.In addition, any combination of two or more such features, systems,articles, materials, kits, and/or methods, if such features, systems,articles, materials, kits, and/or methods are not mutually inconsistent,is included within the scope of the present disclosure.

All definitions, as defined and used herein, should be understood tocontrol over dictionary definitions, definitions in documentsincorporated by reference, and/or ordinary meanings of the definedterms. The indefinite articles “a” and “an,” as used herein in thespecification and in the claims, unless clearly indicated to thecontrary, should be understood to mean “at least one.” The phrase“and/or,” as used herein in the specification and in the claims, shouldbe understood to mean “either or both” of the elements so conjoined,i.e., elements that are conjunctively present in some cases anddisjunctively present in other cases.

Multiple elements listed with “and/or” should be construed in the samefashion, i.e., “one or more” of the elements so conjoined. Otherelements may optionally be present other than the elements specificallyidentified by the “and/or” clause, whether related or unrelated to thoseelements specifically identified. Thus, as a non-limiting example, areference to “A and/or B”, when used in conjunction with open-endedlanguage such as “comprising” can refer, in one embodiment, to A only(optionally including elements other than B); in another embodiment, toB only (optionally including elements other than A); in yet anotherembodiment, to both A and B (optionally including other elements); etc.

As used herein in the specification and in the claims, “or” should beunderstood to have the same meaning as “and/or” as defined above. Forexample, when separating items in a list, “or” or “and/or” shall beinterpreted as being inclusive, i.e., the inclusion of at least one, butalso including more than one, of a number or list of elements, and,optionally, additional unlisted items. Only terms clearly indicated tothe contrary, such as “only one of” or “exactly one of,” or, when usedin the claims, “consisting of,” will refer to the inclusion of exactlyone element of a number or list of elements. In general, the term “or”as used herein shall only be interpreted as indicating exclusivealternatives (i.e. “one or the other but not both”) when preceded byterms of exclusivity, such as “either,” “one of,” “only one of,” or“exactly one of.” “Consisting essentially of,” when used in the claims,shall have its ordinary meaning as used in the field of patent law.

As used herein in the specification and in the claims, the phrase “atleast one,” in reference to a list of one or more elements, should beunderstood to mean at least one element selected from any one or more ofthe elements in the list of elements, but not necessarily including atleast one of each and every element specifically listed within the listof elements and not excluding any combinations of elements in the listof elements. This definition also allows that elements may optionally bepresent other than the elements specifically identified within the listof elements to which the phrase “at least one” refers, whether relatedor unrelated to those elements specifically identified. Thus, as anon-limiting example, “at least one of A and B” (or, equivalently, “atleast one of A or B,” or, equivalently “at least one of A and/or B”) canrefer, in one embodiment, to at least one, optionally including morethan one, A, with no B present (and optionally including elements otherthan B); in another embodiment, to at least one, optionally includingmore than one, B, with no A present (and optionally including elementsother than A); in yet another embodiment, to at least one, optionallyincluding more than one, A, and at least one, optionally including morethan one, B (and optionally including other elements); etc.

It should also be understood that, unless clearly indicated to thecontrary, in any methods claimed herein that include more than one stepor act, the order of the steps or acts of the method is not necessarilylimited to the order in which the steps or acts of the method arerecited.

In the claims, as well as in the specification above, all transitionalphrases such as “comprising,” “including,” “carrying,” “having,”“containing,” “involving,” “holding,” “composed of,” and the like are tobe understood to be open-ended, i.e., to mean including but not limitedto. Only the transitional phrases “consisting of” and “consistingessentially of” shall be closed or semi-closed transitional phrases.

The foregoing description of several methods and embodiments have beenpresented for purposes of illustration. It is not intended to beexhaustive or to limit the precise steps and/or forms disclosed, andobviously many modifications and variations are possible in light of theabove teaching. It is intended that the scope and all equivalents bedefined by the claims appended hereto.

What is claimed is:
 1. A method for producing a hardened and temperedstructural member comprising the steps of: providing a coiled ferrouscontinuous work piece of selected composition; roll forming said coiledferrous continuous work piece into a desired profile; rapidly heatingsaid ferrous continuous work piece in an induction heating device withina range of about 850° C. to 1000° C. within about 300 seconds to produceaustenite substantially throughout the profile of said continuous workpiece; rapidly cooling said austenitized continuous work piece with acooling medium to below about 350° C. within 10 seconds or less toconvert said austenite to martensite substantially throughout saidcontinuous work piece, resulting in a hardened work piece; temperingsaid continuous workpiece by rapidly heating said hardened work piece ina second induction heating device to about 450° 600° C. within 40seconds or less, providing a hardened and tempered work piece of adesired hardness; wherein at least one of said heating, said cooling, orsaid tempering is asymmetrical at selected zones of said work piece;cooling said hardened and tempered continuous work piece to a desiredcutting temperature; and, cutting said hardened and tempered continuouswork piece to a desired length.
 2. The method of claim 1 furthercomprising the step of powder coating said hardened and tempered workpiece.
 3. The method of claim 1 wherein said selected composition ofsaid continuous work piece is SAE 15B27 steel.
 4. The method of claim 1wherein said continuous work piece is subjected to at least one ofsubstantially symmetric heating and symmetric cooling, whereindistortions resulting from different heating or cooling rates issubstantially minimized.
 5. The method of claim 1 wherein saidasymmetrical tempering at one or more zones of said work piece resultsin said hardened and tempered continuous work piece of said desiredprofile having at least a first zone having a first hardness and asecond zone having a second hardness different from said first hardness.6. The method of claim 5 wherein said first zone includes a web.
 7. Themethod of claim 5 wherein said second zone includes at least one flange.8. The method of claim 1 wherein each step occurs substantiallycontinuous and in-line in a straight line.
 9. The method of claim 1wherein distortions are measured by an optical measuring device.
 10. Themethod of claim 9 wherein said optical measuring device includes alaser.
 11. The method of claim 9 wherein said optical measuring devicecontinuously provides measurement information to a computer, and saidcomputer determines if there is distortion above an acceptable amount,wherein said computer activates a calibration device if distortion isabove said acceptable amount.
 12. The method of claim 11 wherein saidmethod further comprises the step of further roll forming said hardenedand tempered continuous work piece resulting from activation of saidcalibration device, and wherein said acceptable amount is less thanabout 1 mm/m.